9M113 Konkurs vs AT-1K Raybolt: Specs Compared

FORCETALLY

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AAnti-tank weapons

AT-1K Raybolt

Anti-tank guided missile

First system

Second system

At a glance

Side by side

Length comparisonOne shared metre scale

9M113 KonkursLength

1.15 m

Length source ↗

AT-1K Raybolt발사관

1.5 m

Length source ↗

Lengths retain their source configuration and measurement scope.

9M113 Konkurslarger figure on 0 of 1

None

AT-1K Rayboltlarger figure on 1 of 1

Speed+178%

Counts only measures both sources give with the same scope. A larger figure is not a better system.

Measured figures

Head to head

16 of 69 rows sourced on both sides

1.15m

1.5m발사관

Length

All recorded figures & sources

1.15 m

Length

Single source

0.875 m

without gas generator

Single source

Configuration

Details

9M113 Konkurs and AT-1K Raybolt configuration
Specification	9M113 Konkurs	AT-1K Raybolt
Crew	—	2 (on foot) 1 (vehicle-mounted)^[source]
Type	Anti-tank missile^[source]	Anti-tank guided missile^[source]
Place of origin	Soviet Union^[source]	South Korea^[source]
In service	1974–present^[source]	—
Used by	See operators^[source]

Wars	Syrian Civil War War in Iraq (2013-2017) War in Donbas Yemeni Civil War (2014-present) Saudi-led intervention in Yemen 2020 Nagorno-Karabakh conflict Russo-Ukrainian War^[source]	Yemeni Civil War Second Nagorno-Karabakh War^[source]

Designed	1970^[source]	2007–2015^[source]

Manufacturer	Tula Machinery Design Bureau (Tula KBP) – Tulsky Oruzheiny Zavod Bharat Dynamics Limited^[source]	Hanwha Vision (launcher) LIG Defense & Aerospace (missile)^[source]

Variants	9M113M^[source]	—

Warhead	2.7 kg (6.0 lb) 9N131 HEAT^[source]	HEAT^[source]

Detonation mechanism	Contact^[source]	Contact fuze^[source]

Engine	Solid-fuel rocket^[source]	—

Guidance system	Wire-guided SACLOS^[source]	Infrared guidance -aided fire-and-forget -^[source]

Steering system	Two control surfaces^[source]	—

Launch platform	Individual, vehicle^[source]	Man-portable launcher^[source]

Former operator · Chechen Republic of Ichkeria	Chechen Republic of Ichkeria^[source]	—

Former operator · East Germany	East Germany^[source]	—

Former operator · Czechoslovakia	Czechoslovakia^[source]	—

Former operator · Finland	Finland^[source]	—

Former operator · Soviet Union	Soviet Union^[source]	—

Source measurement	The original 9M113 with a single-charge warhead can penetrate 600 mm of rolled homogeneous armor (RHA).^[source]9M113 Konkurs · Development; only the objects and conditions stated in this passage The system uses a gas generator to push the missile out of the launch tube. The gas also exits from the rear of the launch tube in a similar manner to a recoilless rifle . The missile leaves the launch tube at 80 meters per second, and is quickly accelerated to 200 meters per second by its solid fuel motor. This initial high speed reduces the missile's deadzone, since it can be launched directly at the target, rather than in an upward arc. In flight, the missile spins at between five and seven revolutions per second.^[source]9M113 Konkurs · Design; only the objects and conditions stated in this passage 9M113M Konkurs-M (NATO: AT-5B Spandrel B ) Tandem warhead – with extended explosive probe. The warhead penetration is 750–800 mm vs RHA. Adopted in 1991. Missile 9M113M 1990. Tandem (800 mm (behind a layer of ERA)). 4,000 m (3500 m night (passive)).^[source]9M113 Konkurs · Models; only the objects and conditions stated in this passage	—

Source measurement

The original 9M113 with a single-charge warhead can penetrate 600 mm of rolled homogeneous armor (RHA).^[source]9M113 Konkurs · Development; only the objects and conditions stated in this passage

The system uses a gas generator to push the missile out of the launch tube. The gas also exits from the rear of the launch tube in a similar manner to a recoilless rifle . The missile leaves the launch tube at 80 meters per second, and is quickly accelerated to 200 meters per second by its solid fuel motor. This initial high speed reduces the missile's deadzone, since it can be launched directly at the target, rather than in an upward arc. In flight, the missile spins at between five and seven revolutions per second.^[source]9M113 Konkurs · Design; only the objects and conditions stated in this passage

9M113M Konkurs-M (NATO: AT-5B Spandrel B ) Tandem warhead – with extended explosive probe. The warhead penetration is 750–800 mm vs RHA. Adopted in 1991. Missile 9M113M 1990. Tandem (800 mm (behind a layer of ERA)). 4,000 m (3500 m night (passive)).^[source]9M113 Konkurs · Models; only the objects and conditions stated in this passage

—

Country of origin	Soviet Union^[source]Inventory Origin column; table 1, row 77, cell 4; revision 1377727163; retrieved 2026-10-02	—

Designer	—	Agency for Defense Development Hanwha Defense (launcher) LIG Nex1 (missile)^[source]

Produced	—	2017–present^[source]

Sights	—	Thermal weapon sight^[source]

Blast yield	—	900 mm (35 in) RHA behind ERA^[source]

Transport	—	4×4 K151C1 ATGM Carrier Rotem KW2 Scorpion Anti-Tank Vehicle^[source]

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